US20100154430A1

US20100154430A1 - System and method for operating a gas turbine using vanadium-containing fuels

Info

Publication number: US20100154430A1
Application number: US12/341,428
Authority: US
Inventors: Krishan Lal Luthra; Henry Stephen Spacil; Jessica W. Spacil
Original assignee: General Electric Co
Current assignee: General Electric Co
Priority date: 2008-12-22
Filing date: 2008-12-22
Publication date: 2010-06-24
Also published as: EP2199569A1; JP2010144728A; CN101806248A

Abstract

A method of operating a gas turbine that utilizes vanadium-containing fuels at a combustion stage of the turbine thereby producing a combustion product having vanadium gaseous species, the method comprising increasing the volatility of the vanadium gaseous species in the combustion product atmosphere generated in a combustor of the turbine by increasing concentration of water vapor in the combustion product.

Description

BACKGROUND OF THE INVENTION

An embodiment of the invention relates to the operation of gas turbines. More specifically, embodiments of the invention relate to gas turbines that are operated using heavy fuels that contain vanadium and/or vanadium species.
Vanadium impurity concentrations in petroleum fuels range from less than 0.5 ppm in distillate fuels to as much as 200 ppm in residual fuels. Corrosion problems associated with liquid vanadium-containing deposits on turbine surfaces limit the use of the cheaper fuels. Present practice is to treat such fuels with magnesium additives which convert the vanadium impurities to solid magnesium vanadates resulting in solid, non-corrosive ash deposits on the blades.
Non-distillate fuels containing more than 2-3 ppm vanadium by weight can be burned in conventional gas turbines only if magnesium or calcium compounds are added to the fuel to form vanadates during combustion. While the liquid vanadium oxide (V₂O₅) and sodium vanadate (NaVO₃) that would otherwise be formed are highly corrosive to gas turbine hot stage materials at moderate temperatures and above, the alkaline earth vanadates (magnesium/calcium vanadates) are solid and result only in deposits within the turbine that are comparatively innocuous from a corrosion standpoint. Solid vanadate-containing deposits can be detrimental to gas turbine operation in other ways, however. First, the deposits decrease aerodynamic efficiency of turbine airfoils, leading to the necessity of periodic removal procedures (“nutshelling” while the turbine is hot, water washing when the turbine is cold). This problem becomes particularly severe for machines with higher firing temperature and high turbine component temperatures where the deposits are hard and difficult to remove by nutshelling and water washing.
Second, higher efficiency gas turbine with firing temperatures approaching 2300° F. depend upon nozzle and bucket cooling by injection of air across the surfaces of these parts (film cooling). Solid vanadate deposits can plug the air cooling ports and lead to overheating of the improperly cooled parts. Thus gas turbines capable of high efficiency operation on clean distillate fuels are generally de-rate for operation on vanadium-containing fuels. Despite these disadvantages, magnesium additives to the fuel are widely used as the only currently feasible approach to utilization of vanadium-containing fuels. No satisfactory method of removing vanadium from fuel prior to combustion has been found. It can be done by setting up or arranging refineries to create distillate fuel which may be complicated and expensive.
Vanadium occurs in the form of soluble porphyrin complex molecules in fuels, but after combustion it would be present in form of gaseous oxides and hydroxides. In most publications, vanadium oxides have been assumed to be the major vanadium containing species in the gas phase. See, W. D. Halstead, Deposition and Corrosion in Gas Turbines, J. Wiley, 1972, p. 22; W. D. Halstead, J. Inst. of Fuel, 42, (1969) 419; and N. S. Bornstein and M. A. DeCrescente, “Properties of High Temperature Alloys,” The Electrochemical Society, Princeton, 1976, p. 626. However, combustion gases in gas turbines contain in excess of 3% H₂O, and at a first stage inlet pressure of greater than 10 atm., the water vapor pressure would be quite significant (>0.3 atm.) resulting in appreciable concentrations of hydroxides. Volatile hydroxides reported in the literature include V₂0₇H₄, VO(OH)₃, VO(OH)₂and VO₂(0H)₂. Glemser and Miiller determined the vapor pressure of V₂O₇H₄by transpiration experiments. See, O. Glemser and A. Muiller, Z. Anorg. Allgem. Chem., 325, (1963) 220. These workers, however, did not demonstrate that their results were in a flow-rate independent region, a necessary experimental condition for equilibrium measurements. Yannoupoulos (912-1172° K) and Taniguchi and Ooue (738-893° K) reported V0(OH)₃to be the predominant vanadium hydroxide while Suito and Gaskell (1173-1373° K) reported VO(OH)₂and V0₂(OH)₂to be the major species. See, L. N. Yannoupoulos, J. Phys. Chem., 72, (1968) 3293; M. Taniguchi and M. Ooue, 23^rd Annual Conf. of the Chem. Soc. of Japan, 1970 Preprint 2, p. 1112; and H. Suito and D. R. Gaskell, “Metal-Slag-Gas Reactions and Processes,” The Electrochemical Society, Princeton, 1975, p. 251. There is a good agreement between the vapor pressure data of Yannoupoulos and Taniguchi and Ooue; the results of Yannoupoulos have been used for the thermodynamic calculations in this work.

BRIEF DESCRIPTION OF THE INVENTION

Disclosed herein are embodiments of the invention for a method of operating a gas turbine that utilizes vanadium-containing fuels. At a combustion stage of the turbine a combustion product having vanadium gaseous species is produced and may result in condensation of vanadium depositions on blades of the turbine. An embodiment of the invention comprises increasing the vapor pressure of the vanadium gaseous species in the combustion product atmosphere generated in the combustor of the turbine by increasing the water vapor pressure of the combustion product. Steam or water vapor may be introduced into the turbine component at location where deposition can occur and cause corrosion of the turbine components; or, the steam/water vapor may be introduced into the combustor. The steam/water vapor may be introduced at locations having moving items such as rotary blades and/or stationary components such as nozzles. Introduction of the steam/water vapor at predetermined temperatures and vapor pressures increases the volatility of the vanadium species. More specifically, vanadium oxide (V₂O₅) and sodium vanadate (Na₂V₂O₅) are oxidized in the presence of the steam/water vapor to form VO(OH)₃and sodium hydroxide (NaOH) gases, which may not as readily condense on the turbine blades forming the solid vanadium depositions.
An embodiment of the invention may also be described as a gas turbine power generation system that comprises a water vapor source in fluid communication with the turbine element for the introduction of the water vapor into the turbine element and/or combustor to increase a vapor pressure of vanadium gaseous species in the combustion product. As noted above, increasing water vapor pressure results in an increase of the vanadium gas species vapor pressure, which may reduce the condensation of the vanadium gaseous species on to hot components of the turbine element. In an embodiment, the system may comprise a closed loop system that takes combustion product and steam (water vapor) exhausted from the turbine element, condenses the gases/vapors into liquid and cleans the liquid, which is then heated and introduced into the turbine element and/or combustor to increase the volatility of the vanadium gaseous species.

BRIEF DESCRIPTION OF THE DRAWINGS

A more particular description of the invention briefly described above will be rendered by reference to specific embodiments thereof that are illustrated in the appended drawings. Understanding that these drawings depict only typical embodiments of the invention and are not therefore to be considered to be limiting of its scope, the invention will be described and explained with additional specificity and detail through the use of the accompanying drawings:

FIG. 1 is a graph illustrating the effect of water vapor concentration on condensate (Na₂V₂O₆—Na₂SO₄—V₂O₅) composition.

FIG. 2 is a graph illustrating effect of water vapor concentration on fuel vanadium tolerance.

FIG. 3 is a schematic illustration representation of the experimental arrangement used for volatilization studies from pure V₂O₅.

FIG. 4 is a schematic illustration representation of the experimental arrangement used for volatilization studies from Na₂V₂O₆—Na₂SO₄—V₂O₅melts.

FIG. 5 is a graph illustrating effect of flow rate of an O₂—H₂O gas mixture on the apparent vapor density of V₂O_5.

FIG. 6 is a graph illustrating effect of P_H ₂ _Oin O₂—H₂O gas mixture on the vapor density of V₂O_5.

FIG. 7 is a graph illustrating effect of P_H ₂ _O(O₂—H₂0-SO₂—SO₃gas mixture) on the volatilization of vanadium from Na₂SO₄—Na₂V₂O₆—V₂O₅melts.

FIG. 8 is a graph illustrating effect of P_H ₂ _O(O₂—H₂0-SO₂—SO₃gas mixture) on the volatilization of vanadium from Na₂SO₄—Na₂V₂O₆—V₂O₅melts.

FIG. 9 is a schematic illustration representation of vanadium volatilization using a steam film cooling process.

DETAILED DESCRIPTION OF THE INVENTION

A more particular description of the invention briefly described above will be rendered by reference to specific embodiments thereof that are illustrated in the appended drawings. Understanding that these drawings depict only typical embodiments of the invention and are not therefore to be considered to be limiting of its scope, the invention will be described and explained.
The major vanadium containing gaseous oxides under turbine conditions are V₂O₅and V₄O₁₀. Yannoupoulos observed that the vapor pressure of vanadium hydroxide was very much greater than that of the oxides in O₂—H₂O mixtures with P_H ₂ _Ogreater than about 0.1 atm. At the reduced activities of V₂O₅expected in condensates (due to association with Na₂O), the vanadium hydroxide vapor pressure would predominate at even lower values of P_H ₂ _O. This follows directly from the individual reactions since:
P_VO(OH) ₃ ⁱ
is proportional to (a_V ₂ _O ₅)^1/2, the vapor pressure of vanadium hydroxide (VO(OH)₃) is proportional to the square root of vanadium oxide activity (a_V ₂ _O ₅)^x, where x equals 1 for V₂O₅and 2 for V₄O₁₀. Thus, vanadium hydroxide is expected to be the major vanadium containing gaseous species in the first stage region of the turbine where P_H ₂ _Ois greater than 0.1 atm.
The formation of VO(OH)₃can be described by the reaction:
V₂O₅ (l)+3H₂O(g)=2V0(OH)₃(g) (1)
The line below V₂O₅indicates that the vanadium oxide can exist in solution at less than unit activity. An increase in water vapor pressure (P_H ₂ _O) would increase the vapor pressure of vanadium compounds and thereby reduce the amount of vanadium in the condensate. Thus, it should be possible to safely use fuels containing higher vanadium impurities by increasing P_H ₂ _Oin the combustion gases.
Thermodynamic calculations have been conducted by the inventors to support this postulate. With respect to FIG. 1, the graph shows the effect of water vapor on the condensate composition at 900° C. For example, for a fuel containing 10 ppm vanadium, the combined sodium vanadate and V₂O₅content of the condensate can be reduced from about 36 mole % to about 0.2 mole % by increasing the steam content in the combustion gases from about 3% for normal operation to about 24%.
In addition, FIG. 2 provides a graphic illustration of the effect of water vapor on the allowable fuel level of vanadium (tolerance limit) to maintain the same total concentration of vanadium in the deposit. For example, if the concentration of H₂O in the gas stream is increased from about 3% to 24%, the concentration of vanadium in the condensate obtained at 900° C. from a fuel containing about 23 ppm vanadium (V) would be about the same as that from a fuel containing 1 ppm V for no enrichment in H₂O. Thus, the tolerance limit is increased from 1 ppm to 23 ppm under these conditions.
Laboratory experiments have been carried out to study the volatilization of vanadium from pure V₂O₅and Na₂V₂O₆—V₂O₅—Na₂SO₄mixtures in the presence of steam. The vapor pressure of vanadium compounds was measured by a transpiration technique. When a carrier gas containing H₂O vapor is passed over vanadium-containing melts at high temperature, the weight of the salt changes due to a loss of vanadium as result of the formation of vanadium hydroxide. Vanadium compounds condense in the cooler parts of the tube due to a decrease in their volatility at lower temperatures. The vapor density of vanadium in the gas stream can be determined by measuring the weight change of the melt as a function of time or by analyzing for the vanadium content of the condensed material.
Volatilization of vanadium from pure V₂O₅was studied using oxygen as the carrier gas. However, for volatilization experiments over Na₂V₂O₆—Na₂SO₄melts, O₂—SO₂mixtures providing SO₃levels typical of gas turbine operating conditions were used. The SO₂—O₂mixture fixes the equilibrium activity of V₂O₅in the melt.
Two kinds of experimental arrangements shown in FIGS. 3 and 4 were used. In the arrangement shown in FIG. 3, P_H ₂ _Oin the O₂—H₂O mixture was controlled by passing O₂first through a water presaturator 10, maintained at a few degrees above the desired temperature, and then through a saturator 12 filled with glass beads at the desired temperature. The glass beads provide a large surface area for equilibration of the gas. The entire section of glass tubing between the presaturator and the furnace tube 14 was heated to above 100° C. to avoid condensation of H₂O. The O₂—H₂O mixture was passed over the salt mixture suspended in a crucible 16 from the arm of a Cahn thermogravimetric balance 18. A thermocouple 20 was provided to monitor or estimate the temperature of the crucible 16. Measurements of the steady state rate of weight loss from the V ₂0₅sample provided the vanadium saturation limit of the gas stream. The experiments, however, had some uncertainties due to steep temperature gradients in the furnace tube and relatively poor (±4° C.) temperature control.
The experimental arrangement shown in FIG. 4 was used for volatilization studies on Na₂V₂O₆—Na₂SO₄—V₂O₅melts. The volatilization experiments were carried out in O₂—SO₂—SO₃—H₂O gas mixtures over a range of water vapor pressures (0-0.83 atm.). The required amount of water vapor was obtained using a syringe pump 22 to inject a controlled flow rate of liquid water through a heated thin capillary 24 of about 0.5 mm internal diameter. The equilibrium value of P_SO ₃was attained by passing the O₂—SO2—H₂O gas mixture over a platinum catalyst 26. The specimen and catalyst were controlled at the same temperature to within ±2° C. After passing over the melt placed in a platinum crucible 28 in the wider section (12 mm i.d.) of the quartz tube 36 (disposed within a furnace 30), the gas mixture passed through the narrow section (6 mm i.d.) where vanadium oxide and vanadyl sulfate condensed (designated with number 32) on the cooler parts. The cooled gas mixture was finally led through a bubbler 34 to the exhaust. After the experiment was over, the condensate in the cooler parts of the tube was dissolved in dilute HF and analyzed for vanadium content.

Results and Discussion

Pure V2O5:
Volatilization of vanadium from pure V₂O₅was studied at 900° C. as a function of gas flow rate and P_H ₂ _O FIG. 5 shows the dependence of vapor density on gas flow rate. Vapor density (v) was obtained from the steady state weight loss rate by the following relation:
$vapor density (μ g of V_{2} O_{5} / litre of gas at STP) = \frac{\begin{matrix} steady state weight \\ loss rate (ug / \min) \end{matrix}}{flow rate (cc / mm)} \times 1000 \times \frac{298}{273}$
The curve for P_H ₂ _O=0.045 illustrates typical effects of varying flow rates. At low flow rates, an erroneously high vapor density is obtained because vapor diffusion from the sample to the cooler sections of the tube contributes significantly to the volatilization rates. At high flow rates, evaporation is too slow to saturate the gas, and an apparently low vapor pressure or vapor density is obtained. The intermediate (plateau) region gives the true equilibrium vapor density. A plot of the results as a function of P_H ₂ _Ois shown in FIG. 5. Yannoupoulos observed a vapor density of 65 ug V/litre (STP) for P_H ₂ _O=0.6 at 900° C., which is in reasonably good agreement with the present value (from FIG. 5) of 140 ug V/litre (STP). It can be seen that the vapor density (or the vapor pressure of vanadium containing species) increases almost linearly with P_H ₂ _O. However, due to the narrow range over which the vapor density was independent of flow rate (FIG. 5), poor control of specimen temperature, and small number of experiments, considerable uncertainty may be associated with the pressure dependence shown. In FIG. 6. Further volatilization experiments were carried out with Na₂SO₄—Na₂V₂O₆—V₂O₅mixtures because of their greater relevance to turbine operation.
Na₂SO₄—Na₂V₂O₆V₂O₅Mixtures
Equilibration Experiments: When a Na₂V₂O₆—Na₂SO₄melt is exposed to O₂—SO₂environments, the salt gains weight as some of the sodium vanadate is converted to V₂O₅. Thermodynamic calculations show that the amount of higher order vanadates (Na₄V₂O₇, Na₆V₂O₈) would he small. The equilibrium between the gas mixture and the melt can be expressed as:
Na₂V₂O₆(1)+SO₃(g)=Na₂SO₄(1)+V₂O₅(1) (2)
In volatilization experiments, Na₂V₂O₆—Na₂SO₄salts were pre-equilibrated with the gas mixture containing the desired level of P_SO ₃The equilibrium composition of the condensate was determined from the weight gain of the salt mixture during equilibration. Table I gives the results of experiments at 750° C. and 900° C. However, the combustion product temperature may range from about 600° C. to about 1100° C. The activity of V₂O₅was calculated from the final composition of the melt, assuming activity coefficient values of one for Na₂SO₄and Na₂V₂O₆and using existing thermodynamic data for Na₂V₂O₆, V₂O₅and Na₂SO₄.
Volatilization Studies: A number of factors are important in volatilization studies from multi-component melts such as those containing Na₂V₂O₆, V₂O₅, and Na₂SO₄:
(1) More than one vapor species may have significant vapor pressures; (2) The loss of components at different rates, e.g., the predominant loss of V₂O₅from Na₂SO₄—Na₂V₂O₆—V₂O₅mixtures, means that the overall composition of the melt changes with time. This difficulty can be circumvented experimentally by using a large quantity of melt and making measurements over a short time span where the overall composition of the melt stays essentially constant; (2) In the presence of a gas that reacts with the melt, e.g., SO₃with Na₂V₂O₆—Na₂SO₄—V₂O₅melt (as in reaction 2), additional weight changes will result even if the bulk composition of the melt stays nearly constant over the duration of experiment; and, (3) In addition to gas phase mass transport limitations that restrict experiments to a maximum flow rate for gas saturation, mass transfer inside the melt may also affect the vaporization kinetics. If mass transfer in the melt is slow relative to vaporization, composition gradients will arise both from the loss of a component and the ingress of compensating gaseous species. Thus, the activity of the evaporating species at the surface may be different from that corresponding to the bulk composition. This problem can be reduced by carrying out experiments at low flow rates so that the volatilization rates are small, but other limitations may arise; for example, the diffusion of vanadium species away from the sample may be faster than the flow of the bulk gas such that an apparently high vapor density is obtained.
An attempt was made to measure by weight changes (for the set up shown in FIG. 3) the rate of volatilization from a Na₂SO₄—Na₂V₂O₆—V₂O₅melt in an O₂—SO₂environment. The experiments were started with Na₂SO₄-50 mole % Na₂V₂O₆(Na₂SO₄-66.6% mole NaVO₃). After an initial period of equilibration with the gas (see reaction 2), the melt experienced a net weight loss which is the result of three major processes which are separate, but related:
$Net weight loss = volatilization of V_{2} O_{5} + volatilization of {Na}_{2} {SO}_{4} - weight gain due to {SO}_{3}$
Corrections for weight loss due to the evaporation of Na₂SO₄are available from existing vapor pressure data and known to those skilled in the art. If the diffusion rate inside the melt is much faster than the volatilization rate, there would be no concentration gradients in the melt and from equation (2) above:
$weight gain due to {SO}_{3} = \frac{80}{182} \times weight loss due to V_{2} O_{5} volatilization,$
and the melt should lose weight at a steady rate.
Analysis of the experimental data showed that the melt did not lose weight steadily and that diffusion inside the melt was affecting the process. As a result, the rate of weight change varied with time, and it was not possible to correct accurately for the weight change due to SO₃pickup by the melt. It was concluded that weight change measurements could not be used to obtain meaningful volatilization rates of vanadium from Na₂SO₄—Na₂V₂O₆—V₂O₅melts.
The experimental arrangement shown in FIG. 4 was adopted as an alternative. Volatilization rates obtained by chemical analysis of condensates in the cooler section of the tube need no correction for the rate of Na₂SO₄loss or weight gain due to SO₃reaction. However, since the rate of volatilization is affected both by flow rate and by the activities of V₂O₅and Na₂SO₄at the surface, which in turn are affected by gas/melt reactions and by interdiffusion in the melt, a flow-rate-independent region may not be obtained.
Table I below gives the results of experiments at 750 and 900° C.

TABLE I

Volatization Studies with Ns₂SO₄—V₂O₅—Na₂V₂O₆

							Vapor
						Total	Density
		Total flow rate			Reaction	Vanadium	(ug V/litre
		at room temp.		Equilibrium	Time	Loss	of gas at
Gas Mixture	P_H ₂ _O	(cc/min.)	Temp. ° C.	P_SO ₃	(Hours)	(ug)	STP

O₂+	0.0	50	750	8.7	24	<6	<0.09
0.15% SO₂
O₂+ 0.2%	0.21	50	750	8.7	57	145	0.93
SO₂
O₂+ 0.2%	0.17	55	750	9.3	66	185	0.92
SO₂
O₂+ 0.4%	0.55	50	750	8.7	41	675	6.00
SO₂
O₂+ 2% SO₂	0.87	50	750	8.7	24	602	9.13
O₂+ 2% SO₂	0.87	50	750	8.7	23.5	625	9.68
O₂+	0.0	50	900	3.7	48	<6	<0.05
0.15% SO₂
O₂+ 0.2%	0.188	50	900	3.7	50	105	0.76
SO₂
O₂+ 0.2%	0.188	50	900	3.7	41.75	65	0.57
SO₂
O₂+ 0.2%	0.188	100	900	3.7	23.75	82	0.63
SO₂
O₂+ 0.2%	0.188	180	900	3.7	21.75	110	0.51
SO₂
O₂+ 0.4%	0.505	50	900	3.7	22	135	2.24
SO₂
O₂+ 2% SO₂	0.84	50	900	3.7	23.25	270	4.23

Most of the experiments were performed at a total gas flow rate of 50 cc/min. it can be seen from the results at 900° C. that under these experimental conditions the gas flow rate had very little effect on volatilization rates.

With respect to FIG. 7 there is graphically shown the inferred values of vapor densities as a function of P_H ₂ _O. It is clear that the vapor density of vanadium increases with P_H ₂ _O. Since the vapor density of vanadium should increase with increasing activity of V₂O₅(reaction 1), the higher vapor density of vanadium at 750° C. than at 900° C. (the combustion product temperature may be between about 600° C. to about 1100° C.) is expected as a result of the higher activity of V₂O₅in the melt, as referenced in Table II below.

TABLE II

Equilibration of Na₂SO₄—50% Na₂V₂O₆mixtures in O₂—0.15% SO₂

		Weight
		of
		starting	Weight
		mixture	gain	Final X	Composition X	X	Calculated a
Temp.° C.	P_SO ₃	(mg)	(mg)	Na₂SO₄	V₂O₅	Na₂V₂O₆	V₂O₅

750	8.74 × 10⁻⁴	199.7	36.7	0.654	0.307	0.04	0.0565
900	3.65 × 10⁻⁴	462.5	41.0	0.583	0.252	0.252	0.0136

The agreement between the experimental vapor density data and the calculated vapor densities using Yannoupoulos' data is extremely good. The experimental vapor density at 750° C. and P_H2O=0.5 atm. is 4 ug V/litre (STP) compared to a value of 3 ug V/litre (STP) obtained by using Yannoupoulos' data and the activity of V₂O₅in table I. Furthermore, for the calculations in FIGS. 1 and 2, VO(OH)₃was assumed to be the predominant vanadium containing gaseous species in the presence of steam; a log-log plot of the experimental vanadium vapor density (FIG. 8) as a function of P_H ₂ _Oshows that the vapor density increases linearly with (P_H ₂ _O)^1.5, which is consistent with VO(OH)₃being the predominant vanadium containing gaseous species.

The theoretical calculations and laboratory experiments discussed above show that by injecting steam into the combustion product atmosphere it should be possible to increase the volatility of vanadium to allow the use of fuels containing higher vanadium levels. To increase the overall P_H ₂ _Oof the combustion gas to effective levels would, however, require unacceptably large quantities of steam. A more practical solution may be to introduce steam locally, where the condensation (and corrosion) problems are encountered. Presently the hot stage components, such as shrouds, blades and vanes of many turbines have air-film cooling. If air cooling is replaced by steam cooling (or air containing steam) a high P_H ₂ _Owould be attained locally at the surface of the blade, and the condensate would be expected to have a reduced vanadium content.
An embodiment of the invention is shown schematically in FIG. 9. V₂O₅and Na₂V₂O₆reaching the blade 38 surface will tend to volatilize in the form of vanadium hydroxide and NaOH by reactions (1) and (3):
Na₂V₂O₆(1)+4H₂O(g)=2VO(OH)₃(g)+2NaOH(g) (3)
In addition to the vanadium volatilization, steam should give better cooling of the blades in comparison to air because of its higher specific heat and thermal conductivity. This approach appears to be directly applicable to present turbines where the blades or vanes have air-film cooling with an add-on system for steam generation. The laboratory experiments with P_H ₂ _Oup to 0.83 atmosphere demonstrate the feasibility of the above approach.
While the preferred embodiments of the present invention have been shown and described herein, it will be obvious that such embodiments are provided by way of example only and not of limitation. Numerous variations, changes and substitutions will occur to those skilled in the art without departing from the teaching of the present invention. For example, if the combustion of the fuel is performed by oxygen or oxygen-enriched air, the concentration and vapor pressure of the water vapor will be higher, and the vanadium tolerance limit will be higher. Accordingly, it is intended that the invention be interpreted within the full spirit and scope of the appended claims.

Claims

1. A method of operating a gas turbine that utilizes vanadium-containing fuels at a combustion stage of the turbine thereby producing a combustion product having vanadium gaseous species, the method comprising:

increasing the volatility of the vanadium gaseous species in the combustion product atmosphere generated in a combustor of the turbine by increasing concentration of water vapor in the combustion product.

2. A method of operating a gas turbine that utilizes vanadium-containing fuels at a combustion stage of the turbine thereby producing a combustion product having vanadium gaseous species, the method comprising:

increasing the vapor pressure of the vanadium gaseous species in a combustion product atmosphere generated in a combustor of the turbine by increasing the water vapor pressure of the combustion product.

3. The method of claim 2, wherein increasing the water vapor includes introducing water vapor to the combustion product at a predetermined temperature and vapor pressure.

4. The method of claim 3, wherein the concentration of water in the combustion product is from about 10% to about 50% by volume with the introduction of the water vapor.

5. The method of claim 3, wherein the concentration of water in the combustion product may range from about 20% to about 40% by volume with the introduction of the water vapor.

6. The method of claim 3, wherein water vapor is introduced to the combustion product at a temperature ranging from about 600° C. to about 1100° C.

7. The method of claim 6, wherein the concentration of water in the combustion product may range from about 20% to about 40% by volume with the introduction of the water vapor.

8. The method of claim 3, wherein water vapor is introduced to the combustion product at a temperature of about 750° C. to 1000° C.

9. The method of claim 8, wherein the concentration of water in the combustion product may range from about 20% to about 40% by volume with the introduction of the water vapor.

10. The method of claim 2, wherein the water vapor pressure of the combustion product is increased directly at a hot stage component such as shroud, vanes, and blades by injecting a water vapor into the turbine element.

11. The method of claim 2, wherein the gas turbine includes a combustor for generating the combustion product that is injected into a turbine element and the step of introducing the water vapor includes introducing the water vapor at the combustor before the combustion product reaches the turbine element.

12. The method of claim 2, further comprising recovering steam and combustion product from the turbine, condensing the steam and combustion products to liquid form, removing impurities from the liquid form and heating the liquid to form steam that is introduced to combustion product for the turbine that has not been combined with water vapor.

13. The method of claim 2, further comprising using a source of liquid oxygen that is injected into a combustor of the gas turbine to produce the combustion product.

14. The method of claim 13, further comprising recovering steam and combustion product from the turbine, condensing the steam and combustion products to liquid form, removing impurities from the liquid form and heating the liquid to form steam that is introduced to combustion product for the turbine that has not been combined with water vapor.

15. The method of claim 14, wherein the water vapor pressure of the combustion product is increased at a stage where the combustion product is injected into a turbine hot stage component such as rotary blades, shroud or vanes.

16. The method of claim 14, wherein the gas turbine includes a combustor for generating the combustion product that is injected into a turbine element and the step of introducing the water vapor includes introducing the water vapor at the combustor before the combustion product reaches the turbine element.

17. The method of claim 2, wherein the vanadium limit of the fuel for the gas turbine is increased by a factor of approximately 10^1.5by increasing the water vapor concentration by a factor of 10.

18. A gas turbine power generation system having a combustor that produces a combustion product that is introduced into a turbine element having a plurality of rotary blades, wherein a vanadium-containing fuel is used at the combustor to produce the combustion product, the system comprising:

a water vapor source in fluid communication with the turbine power generation system for the introduction of the water vapor to the combustion product to increase a concentration of water vapor in the combustion product and reduce condensation of vanadium gaseous species on to the blades in the turbine element.

19. The gas turbine system of claim 18, wherein the water vapor source is in fluid communication with a combustor for introduction of the water vapor to the combustion product.

20. The gas turbine system of claim 18, wherein the water vapor source is in fluid communication with the turbine element such as hot stage component as rotary blades, shrouds or vanes for introduction of the water vapor to the combustion product.

21. The gas turbine system of claim 18, wherein the water vapor is introduced to the combustion at some point on the system prior to the combustion product reaching the turbine element.

22. The gas turbine system of claim 18, wherein the water vapor source comprises a closed loop system in fluid communication with the turbine element comprising one or more conduits for directing water vapor and combustion products from the turbine element to a condenser to condense the water vapor and production products to liquid, then to a heater to heat the liquid and form water vapor that is introduced into the turbine element.